Adaptive position and attitude-tracking controller for satellite proximity operations using dual quaternions
N Filipe, P Tsiotras - Journal of Guidance, Control, and Dynamics, 2015 - arc.aiaa.org
This paper proposes a nonlinear adaptive position and attitude-tracking controller for
satellite proximity operations between a target and a chaser satellite. The controller requires …
satellite proximity operations between a target and a chaser satellite. The controller requires …
Robust fault-tolerant tracking control for spacecraft proximity operations using time-varying sliding mode
The capture of a free-floating tumbling object using an autonomous vehicle is a key
technology for many future orbital missions. Spacecraft proximity operations will play an …
technology for many future orbital missions. Spacecraft proximity operations will play an …
6-DOF robust adaptive terminal sliding mode control for spacecraft formation flying
J Wang, Z Sun - Acta Astronautica, 2012 - Elsevier
This paper addresses the tracking control problem of the leader–follower spacecraft
formation, by which we mean that the relative motion between the leader and the follower is …
formation, by which we mean that the relative motion between the leader and the follower is …
Robust adaptive relative position tracking and attitude synchronization for spacecraft rendezvous
L Sun, W Huo - Aerospace Science and Technology, 2015 - Elsevier
This paper studies the relative position tracking and attitude synchronization of non-
cooperative spacecraft rendezvous with model uncertainty and external disturbance. The …
cooperative spacecraft rendezvous with model uncertainty and external disturbance. The …
Observer-based H∞ fault-tolerant attitude control for satellite with actuator and sensor faults
X Liang, Q Wang, C Hu, C Dong - Aerospace Science and Technology, 2019 - Elsevier
This paper investigates the fault-tolerant attitude stabilization control problem for the satellite
system subject to actuator failures, sensor failures and external disturbances. First, the H∞ …
system subject to actuator failures, sensor failures and external disturbances. First, the H∞ …
Finite-time control for spacecraft formation with dual-number-based description
J Wang, H Liang, Z Sun, S Zhang, M Liu - Journal of Guidance, Control …, 2012 - arc.aiaa.org
SPACECRAFT formation flying (SFF) represents the concept of replacing a complex single
spacecraft with a collective of smaller, less-expensive, and cooperative ones [1, 2]. The SFF …
spacecraft with a collective of smaller, less-expensive, and cooperative ones [1, 2]. The SFF …
Command filtered backstepping-based attitude containment control for spacecraft formation
L Zhao, J Yu, P Shi - IEEE Transactions on Systems, Man, and …, 2019 - ieeexplore.ieee.org
In this paper, the problem of adaptive finite-time attitude containment control for multiple
spacecrafts with unknown external disturbances in spacecraft formation flying is …
spacecrafts with unknown external disturbances in spacecraft formation flying is …
Adaptive sliding mode control for spacecraft proximity operations based on dual quaternions
This paper proposes an adaptive sliding mode control law based on dual quaternions for six-
degree-of-freedom proximity operations between a chaser and a target spacecraft. Dual …
degree-of-freedom proximity operations between a chaser and a target spacecraft. Dual …
Adaptive control on SE (3) for spacecraft pose tracking with harmonic disturbance and input saturation
H Zhang, D Ye, Y Xiao, Z Sun - IEEE Transactions on …, 2022 - ieeexplore.ieee.org
This article investigates the coupled attitude and orbit tracking maneuver control problem of
a spacecraft system in close space missions with model uncertainty, unknown disturbance …
a spacecraft system in close space missions with model uncertainty, unknown disturbance …
Rigid-body attitude stabilization with attitude and angular rate constraints
In this paper, a solution to the problem of rest-to-rest three-axis attitude reorientation of a
fully actuated rigid body under multiple attitude-constraint zones and angular velocity limits …
fully actuated rigid body under multiple attitude-constraint zones and angular velocity limits …